35 satellite platforms, components and ground equipment from manufacturers worldwide.
An upgraded version for KIND34-040. The small-size device for measuring the angular velocity is designed to measure the…
The small-size block for measuring the angular velocity is designed to measure the integrals of the absolute angular…
A laser ranging and velocity measurement system designed for spacecraft, enabling automatic docking by precisely measuring mutual arrangement…
The Reaction Wheels Block is an executive part of a CubeSat three-axis orientation and stabilization system, containing four…
A nanosatellite attitude control unit designed to manage external magnetic coils integrated into solar panels, offering independent PWM…
A magnetic momentum-management system that calms a low-orbit spacecraft and dumps accumulated kinetic moment from the spacecraft body…
An Inertial Measurement Unit (IMU) designed for future manned spacecraft, providing precise measurement of velocity and angle increments…
A redundant, free-form gyroscopic angular velocity vector meter designed for spacecraft orientation and stabilization control systems, measuring angular…
A redundant, free-form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control systems, featuring four fiber-optic…
A three-channel fiber-optic gyroscope sensor designed to measure angular velocity vector projections and transmit this data to a…
A redundant, free-form gyroscopic angular velocity vector meter designed for spacecraft orientation and stabilization control systems, featuring four…
The Kinetic Moment Reset System 1207 is designed to calm low-orbit spacecraft and dissipate accumulated kinetic moment from…
The Electromagnetic Unit (EMU) is a magnetic torquer designed for spacecraft attitude control systems, creating a dipole magnetic…
The Electromagnetic Unit (EMU) is a magnetic torquer for nanosatellites, designed to create a dipole magnetic moment proportional…
The Electromagnet EM-IF-20 is a core electromagnet designed for the stabilization equipment of spacecraft, featuring a harness and…
The Backup Inertial Measuring Device is a sealed monoblock unit designed to measure angular velocities in three axes,…
An Altitude Control System (ACS) designed for spacecraft, providing orientation accuracy of 1 degree and stabilization accuracy of…
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